发明名称 Slew guidance method for spacecraft
摘要 A method is adapted for slewing a body from an initial state to merge with a desired state profile. In an embodiment, the method includes the steps of (a) obtaining data indicative of a time profile of desired future states for the body; (b) searching sequentially through the time profile of desired future states; (c) calculating several slews for the body from the initial state to each of the desired future states; (d) determining the earliest future state to which the body can actually slew; (e) choosing the minimum-energy slew to that state; and (f) causing the body to perform that chosen slew.
申请公布号 US8140198(B1) 申请公布日期 2012.03.20
申请号 US20070934538 申请日期 2007.11.02
申请人 KOENIG JESSE D.;SPACEDEV, INC. 发明人 KOENIG JESSE D.
分类号 G01C23/00;B64G1/14 主分类号 G01C23/00
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